Document Type : Research Paper

Authors

• Amirhossain Adami ¹
• Mehran Nosratollahi ²
• Hanieh Eshagh nia ²
• Sajjad Kheirkhah ³
• Shiva Emami ⁴
• Ali Saadat dar ⁴
• Narges Afsari ⁵
• Khashayar Mashhadi ⁴
• Mansour Hozuri ⁴

¹ Satellite & LV center, Aerospace Department, Malek Ashtar University of Technology.Tehran.IRAN

² Department of Aerospace Engineering, Malek Ashtar University of Technology, Tehran, IRAN

³ Department of Aerospace Engineering, Malek Ashtar University of Technology, Tehran.IRAN

⁴ Department of Aerospace Engineering, Malek Ashtar University of Technology.Tehran.IRAN

⁵ Department of Aerospace Engineering, Malek Ashtar University of Technology, Tehran, Iran.

Abstract

The CANSAT design, a simple and small scale of a satellite, is an experience for preparing for the design of a Life cycle of the space project. In this paper, the process of design and construction of ARTA CanSat, which is participated in the scientific-exploratory class of international competition in CANSAT Iran, has been written. The operation scenario is that an automatic scanner system, lands after releasing from 300 meters above ground level with using a recovery subsystem (parachute), which is controlled its downfall and landing position by the parachute controller system. During the descent, the data is transmitted by the sensors and sent to the ground station. After touchdown, the Hotwire system's operates and separates the parachute from the Rover section; Then CanSat with the moving on the ground by using the simpler section embedded underneath the structure, performing excavation while moving to the target point. Throughout the mission, the health of the biological payload is preserved.

Keywords

• CanSat
• Satellite
• Parachute
• Rover
• Autopilot
• Electrical Motor
• System Design
• Ground Station
• Camera

20.1001.1.20084560.1399.13.2.5.7

Main Subjects

• Space systems design (spacecraft, satellites, space stations and their equipment)